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An experimental investigation of boundary- layer transition on a 10 deg half-angle cone at Mach 6.9Boundary layer transition on nose cones at hypersonic speeds
Document ID
19700015480
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Fischer, M. C. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
April 1, 1970
Subject Category
Fluid Mechanics
Report/Patent Number
L-6940
NASA-TN-D-5766
Report Number: L-6940
Report Number: NASA-TN-D-5766
Accession Number
70N24785
Funding Number(s)
CONTRACT_GRANT: 126-13-10-17-23
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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